Phugoid

Flight Dynamics & Control Workbench

Flight Conditions

Velocity (m/s) Min: 0.1 m/s (Positive value)

Altitude (m) Range: -500 to 50,000 m

Ready for Analysis

Adjust the flight conditions above and calculate to view the trim state and stability modes.

Trim State

Alpha: - deg

Elevator: - deg

Throttle: - %

Theta: - deg

Eigenmodes

Longitudinal Modes

Lateral Modes

Aircraft Attitude

Phugoid

An open-source, serverless flight dynamics and control workbench built for aerospace engineering education and research.

Resources

Documentation
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Created By

Dhruv Haldar

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© 2026 Phugoid Project. MIT Licensed.